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Flight control simulation test method and flight control module

A flight control module and flight control technology, applied in the field of flight control, to achieve the effect of improving efficiency, improving accuracy and improving flexibility

Active Publication Date: 2022-04-12
BEIJING GLOBAL CROWN JINYANG TECH DEV CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, how to drive the flight model of the aircraft to conduct simulation tests according to the working conditions to be tested has become a problem

Method used

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  • Flight control simulation test method and flight control module
  • Flight control simulation test method and flight control module
  • Flight control simulation test method and flight control module

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Embodiment Construction

[0068] The following will clearly and completely describe the technical solutions in the embodiments of the application with reference to the drawings in the embodiments of the application. Apparently, the described embodiments are only some of the embodiments of the application, not all of them. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the scope of protection of this application.

[0069] In order to solve the above problems, the present application provides a flight control simulation test method. Next, the flight control simulation test method provided by the present application will be introduced.

[0070] The flight control simulation test method provided by the application is based on the flight control module, and the flight control module includes: an initialization function and a plurality of flight condition control functions, and each of the flight co...

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Abstract

The invention provides a flight control simulation test method and a flight control module, and the flight control module comprises a flight control module, an initialization function and a plurality of flight condition control functions, and each flight condition control function corresponds to a call sequence. The method comprises the following steps that: a flight control module calls an initialization function to execute the following processes: reading airport information and flight plan information, and outputting aircraft initial state information to a flight model based on the airport information and the flight plan information; when receiving aircraft flight state information fed back by the flight model, the flight control module calls a flight condition control function according to the call sequence, and inputs the aircraft flight state information to the flight condition control function to obtain flight control information; and the flight control module sends the flight control information to the flight model, so that the flight model controls the aircraft to execute a navigation action according to the flight control information.

Description

technical field [0001] The present application relates to the technical field of flight control, in particular to a flight control simulation test method and a flight control module. Background technique [0002] As the technology of aircraft becomes more and more mature, its application scope is also wider and wider, such as map surveying, geological survey, disaster monitoring, patrol inspection and other fields. In order to improve the safety of the automatic flight of the aircraft, it is necessary to conduct a simulation test on the flight model of the aircraft. [0003] However, how to drive the flight model of the aircraft to conduct simulation tests according to the working conditions to be tested has become a problem. Contents of the invention [0004] This application provides the following technical solutions: [0005] On the one hand, the present application provides a flight control simulation test method, based on the flight control module, the flight contro...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B17/02
CPCY02T90/00
Inventor 贝晓狮李京燕李小海
Owner BEIJING GLOBAL CROWN JINYANG TECH DEV CO LTD